| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8918355 | Journal of Space Safety Engineering | 2018 | 12 Pages |
Abstract
Two classical cases are presented to illustrate nutation following fly-around and simulations are implemented to demonstrate the effectiveness of proposed guidance scheme. Further study of proximity mission along spin axis is conducted to show the advantages of guidance scheme.
Related Topics
Physical Sciences and Engineering
Earth and Planetary Sciences
Space and Planetary Science
Authors
Wang Weilin, Song Xumin, Li Kebo, Chen Lei,